Origins nacelle with its distinctive bypass intake nacelle with a conventional intake During the 1950s and 1960s, the French government, which had taken a significant interest in the re-establishment and growth of its national aviation industries in the aftermath of the
Second World War, developed a detailed request for a combined
liaison/
trainer aircraft, to be equipped with twin-turbofan engines. On 4 May 1963, the Mystère 20 prototype, registered
F-WLKB, conducted its
maiden flight from
Bordeaux–Mérignac Airport,
Gironde, France. By this stage, attention in the programme was centered around the commercial opportunities for the type, particularly the large North American market.
Further development A number of Falcon 20s that had been originally powered by CF700 engines were later re-engined with
Garrett TFE731 engines under AMD-BA Service Bulletin No. 731. To distinguish these re-engined aircraft from those still using the original powerplant, they were redesignated with a "-5" suffix inserted after the model number. Volpar Inc. was involved in a program to re-engine the Falcon 20 with the
Pratt & Whitney Canada PW305 engines; however, work on the program was abandoned before a
Federal Aviation Administration (FAA) STC was awarded. An improved model of the aircraft, designated the
Falcon 200, was developed, which featured more advanced jet engines and other major improvements to increase range, capacity, and comfort. The Falcon 200, along with the Falcon 20G and HU-25 models, were powered by a pair of
Garrett ATF3 engines. According to the magazine
Flying, the Falcon 200 variant was more comparable to the newer
Falcon 50 trijet than the original Falcon 20 model. Due to its popularity, Dassault studied and worked upon various variants and extensive derivatives of the Falcon 20. Later-built developments of the type include the smaller
Falcon 10; the larger 30-seat
Falcon 30 with a larger fuselage cross section, which was built and test flown, but did not proceed to production; and the
Falcon 50, an improved three-engined development. The Falcon 20 proved to be so popular that production was not terminated until 1988, when it had been superseded by more advanced developments of the Falcon family. A total of 473 Falcon 20s and 35 Falcon 200s had been constructed by the end of the type's production. During 2013, the FAA modified 14 CFR part 91 rules to prohibit the operation of jets weighing 75,000 pounds or less that were not Stage 3 noise compliant after 31 December 2015. The Falcon 20 was listed explicitly in Federal Register 78 FR 39576. Any examples of the type that had not been modified, either by the installation of Stage 3 noise-compliant engines or have had
hush kits installed upon noncompliant engines, were no longer permitted to fly anywhere in the
contiguous 48 states after 31 December 2015. However,
14 CFR §91.883 Special flight authorizations for jet airplanes weighing 75,000 pounds or less – lists special flight authorizations that may be granted for operation after 31 December 2015. ==Design==